Simulation testing of the shipping package mock-ups under the impact of a falling aircraft engine. Part 2
Authors: Kazantsev A.G., Abramov V.V., Petrov O.M., Radchenko M.V.
Issue: #2 (158)
Mechanics
Model of the explosive traces appearance mechanism in the detonation products
Authors: Andreev S.G., Boiko M.M., Chernov A.I.
Aviation and Rocket-Space Engineering
Comparative analysis of the air conditioning system using the panel and passive heat exchange for a passenger aircraft
Authors: Grishina L.A., Poludnitsyn S.B.
On a possibility of using domestic low-thrust engines in the ultra-low-orbit spacecraft
Authors: Sobolev I.A.
Methods for the mass flowmeters efficient application in technological systems of the spacecraft ground operation
Authors: Bobrovnik V.I., Krasnisheva K.I., Chugunkov V.V.
Quantitative method in assessing the integrity level of composite structures in the helicopter airframe units depending on their design parameters
Authors: Kisin I.D., Zavalov O.A.
Quality control technique of mesh phase separators in fuel tanks of space liquid rocket propulsion units
Authors: Alexandrov L.G., Konstantinov S.B.
Aircraft-type unmanned aerial vehicle control system tuning with a genetic algorithm
Authors: Koshkina A.A., Maslennikov A.L., Babenko M.D., Chulin N.A.